A start/service aircraft battery system including a housing on wheels/dolly for convenient movement to a space adjacent an aircraft to be started/serviced. An electrical output cable is carried by the housing and attachable to the aircraft to be started/serviced. A control panel on the housing includes a start/service switch having a start position and a service position. A starting battery and a larger service battery are carried by the housing, the starting battery being coupled to the electrical output cable through the start/service switch in the start position and the larger service battery being coupled to the electrical output cable through the start/service switch in the service position. The starting battery is removably attached to the start/service aircraft battery system for individual starting operations.

An airport ground power unit for supplying electric current to a parked aircraft and a related system and method. The ground power unit includes a first electric battery, an inverter for transforming an output current of the battery to an alternating output current to be supplied to the aircraft, and one or more first electronic switches for connecting and disconnecting the first battery to and from the inverter. The first switches are connected in serial to the first battery, and together connected to the inverter. A first controller unit controls at least one of the one or more first switches. The ground power unit further includes a second electric battery and second electronic switches for connecting and disconnecting the second battery. The second switches are connected in serial to the second battery and are together connected to the inverter such that they are in parallel to the serially connected first battery and the first switches. At least one of the second switches is controlled by the first or a second digital controller unit.

This specification describes an electrically powered modular platform comprising a power module comprising a common power bus, the power module electrically connected to a power source; one or more service modules that provide a service; a termination module that is configured to cover an opening in the one or more service modules, wherein the power module, each of the one or more service modules, and the termination module are modular and stackable, and wherein the power module and each of the one or more service modules are electrically connected using the common power bus to provide power to each of the one or more service modules.

An unmanned aerial vehicle according to certain embodiments generally includes a chassis, a power supply mounted to the chassis, a control system operable to receive power from the power supply, at least one rotor operable to generate lift under control of the control system, a line having one end coupled to the chassis and an opposite free end, wherein the free end is positioned below the chassis, and a severing mechanism operable to sever the line under control of the control system.

A system for basing drones is described. A network of geographically diverse hangars provides storage and charging locations as well as backhaul communications infrastructure and video monitoring. As drones are needed, a central command point tasks an available drone, which may or may not already be located in proximity to a target. If additional drones are needed, drones can be flown to the area of interest and continuous coverage provided by charging drones while an active drone is conducting the mission, then rotating charged drones into the active mission. Structures for the hangars, the overall system, and methods of operation are described.

A method according to certain embodiments generally involves operating a system including an unmanned aerial vehicle (UAV) and a base station. The base station includes a nest including an upper opening having an upper opening diameter and a lower opening having a lower opening diameter less than the upper opening diameter. The lower opening is accessible from within the base station. The method generally includes landing the UAV within the nest such that a portion of the UAV is accessible via the lower opening, releasably attaching a load to the UAV, and operating the UAV to deliver the load to a destination.

An unmanned aerial vehicle according to certain embodiments generally includes a chassis, a power supply mounted to the chassis, a control system operable to receive power from the power supply, at least one rotor operable to generate lift under control of the control system, a line having one end coupled to the chassis and an opposite free end, wherein the free end is positioned below the chassis, and a severing mechanism operable to sever the line under control of the control system.

An example charging station for an unmanned aerial vehicle (UAV), the charging station generally including a nest and a charging device. The nest includes an upper portion and a lower portion. The upper portion defines an upper opening sized and shaped to receive a landing apparatus of the UAV, and a diameter of the nest reduces from a first diameter at the upper opening to a second diameter at the lower portion. The charging device is mounted in the nest, and includes a first contact pad and a second contact pad. The charging device is configured to apply a voltage differential across the first contact pad and the second contact pad such that the charging station is operable to charge a power supply of the UAV via the landing apparatus.

A container includes a transportation section and a drone section. The drone section has a drone place holder and a door. The drone place holder is accessible when the door is in an open position. The container includes a processor that is programmed to actuate the door to the open position, actuate a drone, fittable in the drone place holder, to fly out of the container, and actuate the drone to transport the container to a destination.

A method according to certain embodiments generally involves operating a system including an unmanned aerial vehicle (UAV) and a base station. The base station includes a nest including an upper opening having an upper opening diameter and a lower opening having a lower opening diameter less than the upper opening diameter. The lower opening is accessible from within the base station. The method generally includes landing the UAV within the nest such that a portion of the UAV is accessible via the lower opening, releasably attaching a load to the UAV, and operating the UAV to deliver the load to a destination.